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AU2004319601B2 - System and method with adaptive angle-of-attack autopilot - Google Patents

System and method with adaptive angle-of-attack autopilot Download PDF

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Publication number
AU2004319601B2
AU2004319601B2 AU2004319601A AU2004319601A AU2004319601B2 AU 2004319601 B2 AU2004319601 B2 AU 2004319601B2 AU 2004319601 A AU2004319601 A AU 2004319601A AU 2004319601 A AU2004319601 A AU 2004319601A AU 2004319601 B2 AU2004319601 B2 AU 2004319601B2
Authority
AU
Australia
Prior art keywords
signal
attack
angle
rate
generate
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
AU2004319601A
Other languages
English (en)
Other versions
AU2004319601A1 (en
Inventor
Keith D. Myers
Edward J. Warkomski
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Co
Original Assignee
Raytheon Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Raytheon Co filed Critical Raytheon Co
Publication of AU2004319601A1 publication Critical patent/AU2004319601A1/en
Application granted granted Critical
Publication of AU2004319601B2 publication Critical patent/AU2004319601B2/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/01—Arrangements thereon for guidance or control
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G05D1/107—Simultaneous control of position or course in three dimensions specially adapted for missiles

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Feedback Control In General (AREA)
AU2004319601A 2003-10-10 2004-10-08 System and method with adaptive angle-of-attack autopilot Ceased AU2004319601B2 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US10/683,518 US7043345B2 (en) 2003-10-10 2003-10-10 System and method with adaptive angle-of-attack autopilot
US10/683,518 2003-10-10
PCT/US2004/033338 WO2005111529A2 (fr) 2003-10-10 2004-10-08 Systeme et procede mis en oeuvre avec un pilote automatique a angle d'attaque adaptatif

Publications (2)

Publication Number Publication Date
AU2004319601A1 AU2004319601A1 (en) 2005-11-24
AU2004319601B2 true AU2004319601B2 (en) 2007-11-22

Family

ID=35134193

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2004319601A Ceased AU2004319601B2 (en) 2003-10-10 2004-10-08 System and method with adaptive angle-of-attack autopilot

Country Status (5)

Country Link
US (1) US7043345B2 (fr)
EP (1) EP1678460B1 (fr)
AU (1) AU2004319601B2 (fr)
IL (1) IL173570A (fr)
WO (1) WO2005111529A2 (fr)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8436283B1 (en) 2008-07-11 2013-05-07 Davidson Technologies Inc. System and method for guiding and controlling a missile using high order sliding mode control
US8346408B2 (en) * 2008-11-10 2013-01-01 The Boeing Company Fault tolerant flight control system
IT1392259B1 (it) * 2008-12-11 2012-02-22 Alenia Aeronautica Spa Procedimento di stima dell'angolo di incidenza e dell'angolo di derapata di un aeromobile
US20120209455A1 (en) * 2011-02-10 2012-08-16 Warkomski Edward J Autopilot with Adaptive Rate/Acceleration Based Damping
US9845146B2 (en) * 2015-10-23 2017-12-19 The Boeing Company Zoom climb prevention system for enhanced performance
CN106406344B (zh) * 2016-09-28 2019-06-04 北京理工大学 一种旋转制导飞行器的增程系统及方法
FR3065543B1 (fr) * 2017-04-19 2019-05-03 Airbus Operations (S.A.S.) Calculateur de commande de vol d'un aeronef
CN108241293B (zh) * 2017-12-08 2020-02-14 中国航空工业集团公司成都飞机设计研究所 一种基于推演导数的过失速机动迎角控制方法
US11029706B2 (en) * 2018-12-07 2021-06-08 The Boeing Company Flight control system for determining a fault based on error between a measured and an estimated angle of attack
US11003196B2 (en) 2018-12-07 2021-05-11 The Boeing Company Flight control system for determining a common mode pneumatic fault
US11066189B2 (en) 2018-12-07 2021-07-20 The Boeing Company Flight control system for determining estimated dynamic pressure based on lift and drag coefficients
CN111361763B (zh) * 2018-12-25 2021-07-13 北京理工大学 能够应用于卫星信号不稳定区域的复合增程飞行器
CN110598294B (zh) * 2019-09-03 2023-05-19 中国航空工业集团公司西安飞机设计研究所 常规布局飞机飞行轨迹稳定性确定方法及装置
CN110928324B (zh) * 2019-12-30 2023-07-14 北京润科通用技术有限公司 无人机飞行参数采集设备及其校准方法
US11577853B2 (en) 2021-04-13 2023-02-14 William M. Fisher Aircraft angle of attack and sideslip angle indicator
CN113849007B (zh) * 2021-09-10 2022-07-26 北京空间飞行器总体设计部 一种用于航天器柔性结构的加速度反馈振动控制方法
CN116039913B (zh) * 2023-02-15 2023-08-22 湖南云箭科技有限公司 航拍固定翼无人机机体抖动的抑制方法及系统

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1986001585A1 (fr) * 1984-09-06 1986-03-13 Affärsverket Ffv Regulateur de servo-commande d'un engin marin

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3594553A (en) * 1969-01-02 1971-07-20 United Control Corp Aircraft instrument
US4234142A (en) * 1978-06-08 1980-11-18 The United States Of America As Represented By The Secretary Of The Navy High angle-of-attack missile control system for aerodynamically controlled missiles
US4609987A (en) * 1983-03-09 1986-09-02 Safe Flight Instrument Corporation Aircraft guidance system for take off or go-around during severe wind shear
US4769759A (en) * 1986-06-16 1988-09-06 Allied-Signal Inc. Method for developing air data for use in flight control systems
US5722620A (en) * 1995-05-15 1998-03-03 The Boeing Company Aircraft pitch-axis stability and command augmentation
US6073065A (en) * 1998-09-04 2000-06-06 Ford Global Technologies, Inc. Method for detecting a bank angle experienced by a moving vehicle
US6131055A (en) * 1998-12-11 2000-10-10 The Boeing Company Aircraft non-normalized angle-of-attack indicating system
US6273370B1 (en) * 1999-11-01 2001-08-14 Lockheed Martin Corporation Method and system for estimation and correction of angle-of-attack and sideslip angle from acceleration measurements

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1986001585A1 (fr) * 1984-09-06 1986-03-13 Affärsverket Ffv Regulateur de servo-commande d'un engin marin

Also Published As

Publication number Publication date
AU2004319601A1 (en) 2005-11-24
WO2005111529A3 (fr) 2006-04-13
WO2005111529A2 (fr) 2005-11-24
US20050278085A1 (en) 2005-12-15
EP1678460B1 (fr) 2015-07-08
IL173570A0 (en) 2006-07-05
EP1678460A2 (fr) 2006-07-12
US7043345B2 (en) 2006-05-09
IL173570A (en) 2010-04-29

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Legal Events

Date Code Title Description
FGA Letters patent sealed or granted (standard patent)
MK14 Patent ceased section 143(a) (annual fees not paid) or expired